Want this question answered?
Wingspan = (perpendicular distance from the tip of the left wing to the fuselage roll-axis) plus (perpendicular distance from the tip of the right wing to the fuselage roll-axis)
the ratio of wing span to the chord of the aerofoil is ASPECT RATIO
Aspect ratio is the ratio of wingspan to chord (front to back of the wing). Alternatively it can be found by (span x span)/ (wing area).
A plane's wingspan is the length of it's wing.
If you had a wing with fixed width and only changed wingspan the aircraft with longer wingspan would produce greater lift. The amount of lift produced by a wing is dependant on many different things but one of those things is wing surface area. Increase the wingspan and you increase area of the wing
The wing spar on this aircraft is one solid assembly tip to wing tip so it is an integral part of the fuselage. This aircraft is not the usual kingair wingbolt bathtub fitting holding the wing on.
There is a component of the total drag of an aircraft called induced drag that depends inversely on the aspect ratio. The length of the wingspan is a key element in calculating aspect ratio. Aspect ratio is defined as the square of the wingspan divided by the wing area. The higher the aspect ratio of the wing, the less induced drag it creates and a slightly higher lift is generated than a shorter aspect ratio wing. In other words, long narrow wings fly easier than short stubby wings, and they stay aloft longer, all other elements being equal. That's one reason commercial jetliners (and the albatross) have such long wings compared to jet fighters (and hawks). That's also how the wingspan of the theoretical rubber engine airplane affects the airborne time of the plane. For an article on aspect ratio from NASA, and a neat little JAVA toy that lets you play with wing parameters, click the link below.
If you are referring to the distance from wing tip to wing tip, it is usually called "wingspan".
Male 37-41 in wingspan. Female 43-50 in wingspan
The wing spar carries the load into the fuselage. The airfoil shape of the wing produces lift which is a force measured in pounds(lbs). This force acts over the surface area of the wing. The structure of the wing with its ribs and skin transfers this load to the wing spar, which transfers it to the fuselage. The spar is like the backbone of the wing.
The wingspan is measured as the distance from wing tip to wing tip. The most common commercial plane, the Boeing, has a wingspan of 107'10"
fuselage centerline is drawn at center of maximum height of the body alined horizontally but fuselage reference line is a zero-lift line of the wing-body of the airplane